IEC TS 62396-1:2006

IEC TS 62396-1:2006

mars 2006
Spécification technique Annulée

Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment

Provides guidance on atmospheric radiation effects on avionics electronics used in aircraft operating at altitudes up to 60 000 feet (18,3 km). Defines the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems. Is intended to help aerospace equipment manufacturers and designers to standardise their approach to single event effects in avionics.

Informations générales

Collections

Normes internationales IEC

Date de publication

mars 2006

Nombre de pages

58 p.

Référence

IEC TS 62396-1:2006

Codes ICS

49.060   Équipements et systèmes électriques aérospatiaux
03.100.50   Production. Gestion de production
31.020   Composants électroniques en général

Numéro de tirage

1 - mai 2006
Résumé
Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment

Provides guidance on atmospheric radiation effects on avionics electronics used in aircraft operating at altitudes up to 60 000 feet (18,3 km). Defines the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems. Is intended to help aerospace equipment manufacturers and designers to standardise their approach to single event effects in avionics.
Norme remplacée par (1)
IEC 62396-1:2012
mai 2012
Norme internationale Annulée
Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment

IEC 62396-1:2012(E) is intended to provide guidance on atmospheric radiation effects on avionics electronics used in aircraft operating at altitudes up to 60 000 feet (18,3 km). It defines the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems. This International Standard is intended to help aerospace equipment manufacturers and designers to standardise their approach to single event effects in avionics by providing guidance, leading to a standard methodology. This International Standard includes the following technical changes with respect to the previous Technical Specification: - Guidance has been provided on the environment for altitudes above 60 000 feet (18,3 km) and the effects on electronics are documented; - a new Annex has been added to provide late news as of 2011 on SEE cross-sections applicable to the atmospheric neutron environment. Keywords: avionics, atmospheric radiation, electronic equipment

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